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This Defense Intelligence Reference Document from the Defense Intelligence Agency, dated 21 November 2010, was produced in FY 2010 under the Advanced Aerospace Weapons System Applications (AAWSA) Program. It reviews propulsion concepts that use plasmas and magnetohydrodynamics. It finds the Ajax MHD energy bypass concept meaningless below Mach 12 but calls a reverse energy bypass with a Virtual Cowl potentially practical. It also predicts that electric propulsion will become standard for spacecraft.
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UNCLASSIFIED/ ,SF&R: &FFI@Iilrt 1!181!! 8HL'I' 2-1 Kuranov and A. Korabelnikov, "Atmospheric Cruise Flight Challenges for Hypersomc Vehicles Under the Ajax Concept,'· Journal of Propulsion and Power, Vol. 24, No. 6. November-December 2008, pp. I 229- 1247. c, D. Riggins, '·Analysis of the Magnethydrodynamic Energy Hypass Engine for High-Speed Airhreathing Propulsion." Journal of Propulsion and Power, Vol. 20. No. 5, 2004, pp.779-792. er, D. Riggins, '·Analysis of the Magnethydrodynamic Energy Hypass Engine for High-Speed Airhreathing Propulsion." Journal of Propulsion and Power, Vol. 20. No. 5, 2004, pp.779-792. c7 Kuranov and A. Korahelnikov, "Atmospheric Cruise Flight Challenges for Hypersonic Vehicles Under the Ajax Concept,"" Journal of Propulsion and Power, Vol. 24, No. 6, Novcmbcr-Dcccmbcr 2008. pp.1229- 1247. 28 Kuranov and A. Korahclnikov, ·'Atmospheric Cruise Flight Challenges for Hypersonic Vehicles Under the Ajax Concept,"" Journal of Propulsion and Power, Vol. 24, No. 6, Novcmbcr-Dcccmbcr 2008. pp.1229- 1247. 29 C. Park. U.B. Mehta, and D.W. Bogdanoff, "Magnetohydrodynamics Energy Bypass Scramjct Perfonnance with Real Gas EllCcts." Journal of Propulsion and Powl:r, Yul. 17. Nu. 5, 2001, pp.1049- 1057. - 10 C. Park. D.W. Bogdanoff~ and U.B. Mehta. "Theoretical Performance of a Magnctohy<lrodynamic- Bypass Scram_jct Engine with Nonequilibrium lo111Lation." Journal of Propulsion and Power, Vol. 19, Nu. 4, 2003, pp. 529-537. 51 M.N. Shneider and S.O. Macheret, "Modeling of Plasma Virtual Shape Control of Ram/Scramjet Inlet and holator," Journal of Propulsion and Power, Vol. 22, No. 2, 2006. pp. 447-454. 52 M.N. Shneider. S.O. Macheret, R.B. Miles. nnd D.M. Van Wie. "MHD Power Generation in Scramjet Engines in Conjunction With Inlet Control:· AIAA 2004-1197. 42nd Aerospace Sciences Meeting and Exhibit, Reno, NV. fanuary 5-8, 2004. 5·' S.O. M.1cheret. M.N. Shneider, .1nd R.B. Miles. "Scr.1rnjet Inlet Control by Off-Body Energy Addition: a Virtual Cowl.'" AIAA Journal, Vol. 42, No. I I, November 2004, pp. 2294-2302. i-1 M.N. Shneider, S.O. Macheret. S.H. Zaidi, I. Girgis. and R.B. Miles, ·'Virtual Shapes in Supersonic Flow Control with Energy Addition."' Journal of Propulsion and Power. Vol. 25, No.5, 2008. pp. 900-915. 1"' S.O. Macheret, M.N. Shneider. and R.B. Miles, "Scramjet Inlet Control by Off-Body Energy Addition: a Virtual Cowl.'" AIAA Journal, Vol. 42, No. I I, November 2004, pp. 2294-2302. 11' M.N. Shneider, S.O. Macheret, S.H. Zaidi, I. Girgis, and R.B. Miles. '"Virtual Shapes in Supersonic Flov.' Control with Energy Addition,"' .Journal of Propulsion and Pmvl:r, Vol. 25, No.5. 2008. pp. 900-915. • 17 S.O. MachcrL:t, M.N. ShnL:idcr, and G.V. Candler. "Modeling ofMHD Power Grncration On Board Reentry Vehicles," AIAA 2004-1024, 42nd Acro~pacc Sciences Meeting and Exhihit. Reno, NV, January 5-8, 2004. • 18 C. StL:cvcs, M.N. ShnL:idcr, S.O. MaL:hcrct. R.B. Miles, H. Wadley, and A. Evans, ·'Electrode Design for Magnctohydrodynamic Power Panels on Rc-EntL:ring SpaL:c VL:hielcs,"' Papl:r AIAA-2005-1340. 43rd AIAA Acrospm.T ScirnLTs ML:cting and Exhibit. Reno, Nevada, Jan. 10- I 3, 2005. - 1~ N. Barlow. C. Steeves, M. ShncidL:r, S. MacbL:rl:\, R. Miks, and A. Evans, "Mod ding of Near-Electrode Layers for MIID Power Panels on Reentering Space VL:hiclcs,"' Paper AIAA 2005-5047, 36th AIAA Plasmadynamics and Lasers ConfcrL:ncc, Toronto, Ontario, Canada, 6-9 Junl: 2005. 40 T. Wan. G. Candler, S. MachercL and M. Slmeidcr, "Thrcc-DimL:nsional Simulation of the Ekctric Field and Magnetohydrodynamic Power Generation during Reentry," AIAA Joum.11. Vol. 47, No. 6. 2009, pp. 1327- 1336. 41 S.O. M.1cheret. M.N. Shneider, and G.V. Candler. "Modeling of MHD Power Generation On Board Reentry Vehicles," AIAA 2004-1024, 42nd Aerospace Science~ Meeting and Exhibit, Reno, NV. January 5-8. 2004. 42 I.G. Girgis, M.N. Slmeider, S.O. Macheret, G.L. Brown, and R.B. Miles, "Creation of Steering Moments in Supersonic Flow by Off-Axis Plasma Heat Addition,'· Journal of Spacecraft and Rockets, Vol. 43, No. 3. 2006. pp. 607-613. -1-1 R. Litchford et al., "Magnetohydrodynamic Augmented Propulsion Experiment: I. Performance Analysis and Design.'· AIAA 2002-2184, 33rd PlasmadynamiL:s and Laser Conference, Mam. HI, May 2002. -1-1 R. Litchford and J. Lineberry, ··status of Magneto hydrodynamic Augmented Propulsion Experiment.'" AIAA-2007-3884, 38th AIAA Plasmadynamics and Lasers Conference, Miami, FL June 2007. UNCLASSIFIED/f8R 8ffl@Iilrt 1!191!! 8HLV 27
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Report, from the dia collection. The PDF is mirrored here; the original link is above. 32 pages are in the text index: search them above, or from the library's search.